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39篇 您的检索式：作者名="TSOURDOS A"

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	题名	作者	年代	出处	被引量
1	Quasilinear Parameter-Varying Autopilot Design Using Polynomial Eigenstructure Assignment with Actuator Constraints显示文摘	Bruyere L Tsourdos A White B A	2006	Journal of Guidance Control and Dynamics2006，29，6：	1
2	Differential geomet- ric guidance based on the involute of the target ~s trajectory 显示文摘	Ariff O Zbikowski R Tsourdos A	2005	Journal of Guidance Control and Dynamics2005，28，5：	1
3	Adaptive flight control designfor nonlinear missile显示文摘	Tsourdos A White B A	2005	Control Engineering Practice2005，13，：	1
4	Robust covariance estimation for data fusion from multiple sensors显示文摘	Sequeira J Tsourdos A Lazarus S B		0，，12：	1
5	Contaminant cloud boundary monitoring using network of UAV sensors显示文摘	White B A Tsourdos A Ashokaraj I	2008	Sensors Journal2008，8，10：	1
6	Polynomial approach for design and robust analysis of lateral missile control 显示文摘	Bruyere L Tsourdos A White BA	2006	International Journal of Systems Science2006，37，8：	1
7	Nonlinear relative posi- tion control of precise formation flying using polynomial eigen- structure assignment显示文摘	Wang F Chen X Q Tsourdos A	2011	Acta Astronautica2011，68，1112：	1
8	Missile autopilot design using quasi-LPV polynomial eigenstructure assignment显示文摘	White B A Bruyere L Tsourdos A	2007	IEEE Transactions on Aerospace and Electronic Systems2007，43，4：	1
9	Adaptive flight control design for nonlinear missile显示文摘	TSOURDOS A WHITE B A	2005	Control Engineering Practice2005，13，3：	1
10	Adaptive flight control design for nonlinear missile 显示文摘	Tsourdos A Brian A	2005	Control Engineering Practice2005，13，3：	1
11	查看详情显示文摘	A Tsourdos B A White		0，，：	1
12	Differential geometric guidance based on the involute of the target’s trajectory 显示文摘	Ariff O Zbikowski R Tsourdos A	2005	Journal of Guidance Control and Dynamics2005，28，5：	1
13	Differential geometric guidance based on the involute of the target's trajectory显示文摘	Zbikowski R Tsourdos A	2005	Journal of Guidance Control and Dynamics2005，28，5：	1
14	Missile autopilot design using quasi-LPV polynomial eigenstructure assignment 显示文摘	Bruye're L Tsourdos A White B	2007	IEEE Transactions on Aerospace and Electronic Systems2007，43，4：	1
15	Missile autopilot design with actuator limitations: a polynomial eigenstructure assignment approach显示文摘	Bruyere L Tsourdos A White B	2006	Journal of Guidance Control and Dynamics2006，29，6：	1
16	Adaptive flight control design for nonlinear missile 显示文摘	Tsourdos Antonios White B A	2005	Control Engineering Practice2005，13，3：	1
17	Optimal impact angle con- trol guidance law based on linearization about collision triangle 显示文摘	Cho H Ryoo C K Tsourdos A	2014	Journal of Guidance Control and Dynamics2014，37，3：	1
18	Cooperative path planning of multiple UAVs using Dubins paths with clothoid arcs显示文摘	Shanmugavel M Tsourdos A White B	2010	Control Engineering Practice2010，18，9：	1
19	Nonlinear model predictive coordi- nated standoff tracking of a moving ground vehicle 显示文摘	KIM S OH H TSOURDOS A	2013	Journal of Guidance Control and Dynamics2013，36，2：	1
20	Cooperative path planning of multiple UAVs using Dubins paths with clothoid arcs 显示文摘	SHANMUGAVEL M TSOURDOS A WHITE B	2010	Control Engineering Practice2010，18，9：	1

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